5. The vector valued function rm = rco3[mt]i + raln[mc]j will trace out the path of a satellite in the circular orbit. Here r is the radius of the circle and to is the angular speed. We refer to t) as a position vector for the satellite {it} Find a vector valued function for the velocity of the satellite. {I}! Find a vector valued function for the acceleration of the satellite. [c] Show that, In circular motion, the velocity vector ls perpendicular to the position vector lav computing the dot product ofthe veloch and position vectors